EP3310838B1 - Epoxy resin composition - Google Patents

Epoxy resin composition Download PDF

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Publication number
EP3310838B1
EP3310838B1 EP16730283.5A EP16730283A EP3310838B1 EP 3310838 B1 EP3310838 B1 EP 3310838B1 EP 16730283 A EP16730283 A EP 16730283A EP 3310838 B1 EP3310838 B1 EP 3310838B1
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Prior art keywords
composition according
component
bis
epoxy resin
alkyl
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German (de)
French (fr)
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EP3310838A1 (en
Inventor
Christian Beisele
Werner Hollstein
Andreas RIEGGER
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Huntsman Advanced Materials Licensing Switzerland GmbH
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Huntsman Advanced Materials Licensing Switzerland GmbH
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/20Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
    • C08G59/32Epoxy compounds containing three or more epoxy groups
    • C08G59/3218Carbocyclic compounds
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/68Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/68Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used
    • C08G59/686Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used containing nitrogen
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/01Use of inorganic substances as compounding ingredients characterized by their specific function
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20Oxides; Hydroxides
    • C08K3/22Oxides; Hydroxides of metals
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/34Silicon-containing compounds
    • C08K3/36Silica
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K9/00Use of pretreated ingredients
    • C08K9/04Ingredients treated with organic substances
    • C08K9/06Ingredients treated with organic substances with silicon-containing compounds
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09DCOATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D163/00Coating compositions based on epoxy resins; Coating compositions based on derivatives of epoxy resins
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B3/00Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties
    • H01B3/18Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances
    • H01B3/30Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes
    • H01B3/40Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes epoxy resins
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20Oxides; Hydroxides
    • C08K3/22Oxides; Hydroxides of metals
    • C08K2003/2265Oxides; Hydroxides of metals of iron
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/002Physical properties
    • C08K2201/005Additives being defined by their particle size in general
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/011Nanostructured additives
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/014Additives containing two or more different additives of the same subgroup in C08K

Definitions

  • the present invention relates to a curable composition
  • a curable composition comprising an epoxy resin and a filler composition, a cured product obtained by curing said curable composition as well as the use of the curable composition as insulating material for electrical and electronic components, in particular as encapsulation system for printed circuit boards.
  • EP 2 868 692 A1 is directed to a stabilized matrix-filled liquid radiation curable resin composition for additive fabrication including a cationically polymerizable component that is an aliphatic epoxide, a multifunctional (meth)acrylate component, a cationic photoinitiator, a free-radical photoinitiator, and a matrix of inorganic fillers, wherein the matrix constitutes prescribed ratios of at least one microparticle constituent and at least one nanoparticle constituent.
  • the invention relates to a composition
  • a composition comprising
  • epoxy resins suitable as component (a) are those customary in epoxy resin technology.
  • examples of epoxy resins are:
  • epoxy resins wherein the 1,2-epoxy groups are bonded to different hetero atoms or functional groups; such compounds include, for example, the N,N,O-triglycidyl derivative of 4-aminophenol, the glycidyl ether glycidyl ester of salicylic acid, N-glycidyl-N'-(2-glycidyloxypropyl)-5,5-dimethylhydantoin and 2-glycidyloxy-1,3-bis(5,5-dimethyl-l-glycidylhydantoin-3-yl)propane.
  • such compounds include, for example, the N,N,O-triglycidyl derivative of 4-aminophenol, the glycidyl ether glycidyl ester of salicylic acid, N-glycidyl-N'-(2-glycidyloxypropyl)-5,5-dimethylhydantoin and 2-glycidyloxy-1,3-bis
  • component (a) is a cycloaliphatic epoxy resin.
  • cycloaliphatic epoxy resin in the context of this invention denotes any epoxy resin having cycloaliphatic structural units, that is to say it includes both cycloaliphatic glycidyl compounds and ā‡ -methylglycidyl compounds as well as epoxy resins based on cycloalkylene oxides.
  • Suitable cycloaliphatic glycidyl compounds and ā‡ -methylglycidyl compounds are the glycidyl esters and ā‡ -methylglycidyl esters of cycloaliphatic polycarboxylic acids, such as tetrahydrophthalic acid, 4-methyltetrahydrophthalic acid, hexahydrophthalic acid, 3-methylhexahydrophthalic acid and 4-methylhexahydrophthalic acid.
  • cycloaliphatic epoxy resins are the diglycidyl ethers and ā‡ -methylglycidyl ethers of cycloaliphatic alcohols, such as 1,2-dihydroxycyclohexane, 1,3-dihydroxycyclohexane and 1,4-dihydroxycyclohexane, 1,4-cyclohexanedimethanol, 1,1-bis(hydroxymethyl) cyclohex-3-ene, bis(4-hydroxycyclohexyl)methane, 2,2-bis(4-hydroxycyclohexyl)propane and bis(4-hydroxycyclohexyl)sulfone.
  • cycloaliphatic alcohols such as 1,2-dihydroxycyclohexane, 1,3-dihydroxycyclohexane and 1,4-dihydroxycyclohexane, 1,4-cyclohexanedimethanol, 1,1-bis(hydroxymethyl) cyclohex-3-ene, bis(4-hydroxycyclohex
  • epoxy resins having cycloalkylene oxide structures are bis(2,3-epoxycyclopentyl)ether, 2,3-epoxycyclopentylglycidyl ether, 1,2-bis(2,3-epoxycyclopentyl)ethane, vinyl cyclohexene dioxide, 3,4-epoxycyclohexylmethyl 3',4'-epoxycyclohexanecarboxylate, 3,4-epoxy-6-methylcyclohexylmethyl-3 ',4'-epoxy-6'-methylcyclohexanecarboxylate, bis(3,4-epoxycyclohexylmethyl)adipate and bis(3,4-epoxy-6-methylcyclohexylmethyl)adipate.
  • the composition according to the invention contains as component (a) a cycloaliphatic epoxy resin selected from bis(4-hydroxycyclohexyl)methane-diglycidyl ether, 2,2-bis(4-hydroxycyclohexyl)propanediglycidyl ether, tetrahydrophthalic acid diglycidyl ester, 4-methyltetrahydrophthalic acid diglycidyl ester, 4-methylhexahydrophthalic acid diglycidyl ester and, in particular, 3,4-epoxycyclohexylmethyl3',4'-epoxycyclohexanecarboxylate.
  • a cycloaliphatic epoxy resin selected from bis(4-hydroxycyclohexyl)methane-diglycidyl ether, 2,2-bis(4-hydroxycyclohexyl)propanediglycidyl ether, tetrahydrophthalic acid diglycidyl ester, 4-methyltetrahydrophthalic acid dig
  • initiator system for the cationic polymerisation of the epoxy resin there is used a mixture comprising
  • compositions according to the invention contain as component (b1) a quaternary ammonium salt with an aromatic heterocyclic cation of formula (1), (2) or (3) wherein R 1 is C 1 -C 12 alkyl, C 7 -C 36 aralkyl, C 3 -C 15 alkoxyalkyl or benzoylmethyl, R 2 , R 3 , R 4 , R 5 and R 6 independently of the other are hydrogen, C 1 -C 4 alkyl or phenyl or R 2 and R 3 or R 3 and R 4 or R 4 and R 5 or R 5 and R 6 together with the carbon atoms to which they are attached form a benzene, naphthalene, pyridine or quinoline ring.
  • component (b1) a quaternary ammonium salt with an aromatic heterocyclic cation of formula (1), (2) or (3) wherein R 1 is C 1 -C 12 alkyl, C 7 -C 36 aralkyl, C 3 -C 15 alkoxyalkyl
  • radicals R 1 - R 6 When any of the radicals R 1 - R 6 is alkyl, that radical or those radicals may be straight-chain or branched.
  • alkyl groups are methyl, ethyl, n-propyl, isopropyl, n-butyl, isobutyl, sec-butyl, tert-butyl, n-pentyl, neopentyl, n-hexyl, n-heptyl, n-octyl, isooctyl, n-decyl and n-dodecyl.
  • Aralkyl groups as R 1 have preferably from 7 to 30 carbon atoms, especially from 7 to 12 carbon atoms.
  • Suitable aralkyl groups are benzyl, 2-phenylethyl, tolylmethyl, mesitylmethyl and 4-chlorophenylmethyl.
  • alkoxyalkyl groups are 2-methoxyethyl, 3-methoxypropyl, 4-methoxybutyl, 6-methoxyhexyl, 2-ethoxyethyl, 3-ethoxypropyl, 4-ethoxybutyl and 6-methoxyhexyl.
  • the composiztions contain as component (b1) a quaternary ammonium salt of formula (4) wherein R 7 denotes methyl, ethyl, n-butyl, benzyl or benzoylmethyl, and Z - is hexafluorophosphate, hexafluoroarsenate, hexafluoroantimonate, pentafluorohydroxyantimonate, tetrafluoroborate, tetrakis[3,5-bis(trifluoromethyl)-phenyl]borate and tetrakis(pentafluorophenyl)borate.
  • R 7 denotes methyl, ethyl, n-butyl, benzyl or benzoylmethyl
  • Z - is hexafluorophosphate, hexafluoroarsenate, hexafluoroantimonate, pentafluorohydroxyantimonate, tetrafluoroborate,
  • suitable compounds of the formula (4) are N-methylquinolinium hexafluorophosphate, N-methylquinolinium hexafluoroarsenate, N-methylquinolinium hexafluoroantimonate, N-methylquinolinium pentafluorohydroxyantimonate, N-methylquinolinium tetrafluoroborate, N-methylquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate, N-methylquinolinium tetrakis(pentafluorophenyl)borate, N-ethylquinolinium hexafluorophosphate, N-ethylquinolinium hexafluoroarsenate, N-ethylquinolinium hexafluoroantimonate, N-ethylquinolinium pentafluorohydroxyantimonate, N-ethylquinolinium tetrafluoroborate, N-ethylquinolini
  • the most preferred compound of the formula (4) is N-benzylquinolinium hexafluoroantimonate.
  • (b2) is a compound of formula (5) wherein R 8 , R 9 , R 10 and R 11 independently of the other are phenyl that is unsubstituted or substituted by C 1 -C 12 alkyl, C 1 -C 12 alkoxy, C 7 -C 36 aralkyl, C 6 -C 36 aryl, C 3 -C 15 alkoxyalkyl, C 1 -C 12 alkylthio, C 1 -C 12 alkylcarbonyl, halogen, nitro or cyano, and R 12 and R 13 independently of the other are hydrogen or C 1 -C 12 alkyl.
  • Examples for suitable compounds of formula (5) are 1,2-bis(2-methylphenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2-ethylphenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2-fluorophenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2,6-difluorophenyl)-1,2-diphenyl-1,2-ethanediol and, in particular, 1,1,2,2-tetraphenyl-1,2-ethanediol.
  • compositions according to the invention optionally comprise a curing accelerator as additional component.
  • Suitable accelerators are known to the person skilled in the art. Examples that may be mentioned are:
  • Preferred accelerators are imidazoles, in particular N-methylimidazole.
  • An essential component of the curable composition according to the present invention is a filler composition comprising a microparticle filler and a nanoparticle filler.
  • the microparticle filler is preferably selected from globular or angular metal or semi-metal oxides, nitrides, carbides and hydroxides, especially from the goup consisting of silica flour, amorphous silica (natural amorphous silica or fused silica), aluminium oxide, silicon carbide, boron nitride, aluminium nitride, aluminium hydroxide and magnesium hydroxide.
  • the microparticles have an average particle size (d 50 ) of 1 to 100 ā‡ m, more preferably from 2 to 50 ā‡ m and most preferably from 5 to 25 ā‡ m determined according to ISO 13320-1:1999.
  • Component (c) of the compositions according to the invention is preferably amorphous silica.
  • the amorphous silica is natural amorphous silica or fused silica.
  • Fused silica with an average particle size (d 50 ) of 10.5 ā‡ m is commercially available under the name TECOSILĀ® from CE Minerals, Greenville, TN, USA.
  • Natural amorphous silica is available under the name AMOSILĀ® from Quarzwerke, Germany.
  • the amorphous silica has an average particle size d 50 of 1 to 100 ā‡ m, more preferably from 2 to 50 ā‡ m and most preferably from 5 to 25 ā‡ m determined according to ISO 13320-1:1999.
  • the amorphous silica is surface treated.
  • the amorphous silica is surface treated with a silane, more preferably selected from the group consisting of amino silane, epoxy silane, (meth)acrylic silane, methyl silane and vinyl silane.
  • the silane is a compound of the following formula: wherein R denotes methyl or ethyl.
  • the nanoparticle fillers are preferably selected from oxides, carbonates, nitrides and silicates of magnesium, calcium, boron, aluminium and silicon.
  • nanoparticle fillers essentially consist of calcium carbonate, boron nitride, montmorillonite or silicon dioxide.
  • Silica nanoparticles are particularly preferred.
  • the preparation of silicon dioxide nanoparticles is disclosed, for example, in WO 02/083776 .
  • the preferred silicon dixide nanoparticles are substantially spherical and have only slight, if any, agglomeration and/or aggregation.
  • the nanoparticles are preferably surface-modified in order to prevent or reduce their agglomeration.
  • a preferred surface modification is silanization with appropriate silanes, for examples the silanes mentioned above as surface modification agents for silica microparticles.
  • nanoparticle fillers are known and to some extent commercially available, for example under the designation NANOPOXĀ® (supplied by Evonik).
  • a preferred nanop architecture filler is NANOPOXĀ® E 601, which is a dispersion of silica nanoparticles in a cycloaliphatic epoxy resin.
  • the average particle size of the silica nanoparticles d 50 is usually between 2 and 100 nm, preferably between 6 and 40 nm, more preferably between 8 and 80 nm and in particular between 10 and 25 nm.
  • D 50 is known as the medium value of particle diameter. This means that a powder comprises 50% of particles having a larger particle size and 50% of particles having a smaller particle size than the dso value.
  • the relative amounts of components (a), (b), (c) and (d) may vary within wide ranges.
  • the total amount of filler (c) + (d) is 60 to 90 % by weight, preferably 65 to 85 % by weight and in particular 70 - 80 % by weight based on the total composition (a) + (b) + (c) + (d).
  • the amount of microparticle filler (c) is 55 to 80 % by weight, more preferably 60 to 75 % by weight and in particular 65 to 70 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • the amount of nanoparticle filler (d) is 2 to 20 % by weight, more preferably 5 to 15 % by weight and in particular 7 to 12 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • the amount of cationically polymerisable epoxy resin (a) is preferably 10 to 40 % by weight, more preferably 15 to 30 % by weight and in particular 20 to 25 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • the amount of initiator for the cationic polymerisation initiator (b) is preferably 0.05 to 1.0 % by weight, more preferably 0.1 to 0.7 % by weight and in particular 0.2 to 0.5 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • the curable composition according to the present invention can additionally comprise further additives, such as flexibilizers, thixotropic agents, wetting agents, antisettling agents, colour agents, defoamers, light stabilizers, mold release agents, toughening agents, adhesion promoters, flame retardants, curing accelerators, etc.
  • further additives such as flexibilizers, thixotropic agents, wetting agents, antisettling agents, colour agents, defoamers, light stabilizers, mold release agents, toughening agents, adhesion promoters, flame retardants, curing accelerators, etc.
  • compositions according to the present invention are heat-curable mixtures.
  • the cationically polymerisable epoxy resin (a) is mixed with the required amount of the initiator for the cationic polymerisation (b).
  • These mixtures are stable at room temperature and can be handled without hazard. In general, it is not necessary to add any additional activating component prior to initiation of polymerisation, so that the mixtures are one-component systems which can be cured at any time.
  • the polymerisation is initiated by heating the the mixture to temperatures of 60 - 220 Ā°C, preferably 80 - 200 Ā°C and in particular 100 .- 190 Ā°C, depending on the material used and the desired polymerisation time.
  • the cured products demonstrate surprisingly excellent mechanical properties, in particular with respect to thermal stability and crack resistance.
  • a further embodiment of the present invention is a cured product which is obtainable by curing a curable composition according to the present invention.
  • the cured products according to the present invention are preferably used as electrically insulating construction material for electrical or electronic components.
  • the curable compositions according to the invention can specifically be applied as casting system for medium to high voltage applications, e.g for insulators, bushings, transformers, instrument transformers and switchgears, in all cases for indoor as well as outdoor applications, especially as encapsulation systems for printed circuit boards.
  • the curable compositions according to the invention may be used as encapsulation material for stators and rotors of electrical machines such as motors or generators. They may be used either as full encapsulation systems or only for impregnation of the end turns of the windings.
  • a further embodiment of the present invention is a method for the manufacturing of electrical insulation equipment comprising the steps:
  • the invention further relates to the use of the composition according to the invention as insulating material for electrical and electronic components.
  • composition according to the invention is used as encapsulation system for printed circuit boards.
  • a further embodiment of the present invention is the use of the curable compositions as adhesives.
  • Tensile strength and elongation at break are determined at 23 Ā°C according to ISO R527 K IC (critical stress intensity factor) in MPa ā€¢ m and G IC (specific break energy) in J/m 2 are determined at 23 Ā°C by double torsion experiment (Huntsman-internal method).
  • CTE coefficient of linear thermal expansion
  • T g glass transition temperature
  • SCT Crack index (simulated crack temperature) is calculated based on T g , G IC , CTE and elongation at break according to the description given in WO 00/55254 .
  • ARALDITEĀ® XB 5992 100 g of ARALDITEĀ® XB 5992 are mixed with 90 g of ARALDITE XB 5993 and the mixture is heated while slightly stirring with a propeller stirrer to about 60 Ā°C for about 5 minutes. Then the mixer is stopped and 2 g of BAYFERROXĀ® 225 is added and the mixer is started again for about 1 min. Subsequently, while stirring, 51.3 g of TREMINĀ® 283-600 EST and 290.7 g of AMOSILĀ® 520 are added in portions and the mixture is heated up to 60 Ā°C under stirring for about 10 minutes. Then the mixer is stopped and the vessel is degassed carefully by applying a vacuum for about 1 minute.
  • the mixture is poured into a 140 Ā°C hot steel mold to prepare plates for the determination of the properties (4 mm thickness).
  • the mold is then put to an oven for 30 minutes at 140Ā°C. After thermally curing the mold, the mold is taken out of the oven and the plates are cooled down to ambient temperature (25Ā°C).
  • the results of the tests are summarised in Table 1.
  • Table 1 The amounts of the ingredients of Compositions A1, C1 and C2 are given in parts by weight Composition A1 C1 C2 ARALDITEĀ® CY 179-1 9.60 ARALDITEĀ® XB 5992 18.73 INITIATOR 1 0.13 CO-INITIATOR 1 0.17 ARALDITEĀ® XB 5993 16.85 ARADURĀ® HY 906 17.33 ACCELERATOR 1 0.15 NANOPOXĀ® E 601 22.50 23.03 AEROSILĀ® R 972 0.20 0.55 AMOSILĀ® 510 21.75 33.65 AMOSILĀ® 520 44.73 54.44 24.24 TREMINĀ® 283-600 9.61 BYK W 940 0.50 0.20 BYK W 995 0.12 BYK 070 0.21 0.15 SILFOAMĀ® SH 0.21 0.09 SILAN A-187 0.50 BAYFERROXĀ® 225 0.37 Viscosity at 60 Ā°C/Pa ā‡ s 15 8.6 5 Curing conditions 1h/120 Ā°C 30 min/140 Ā°C
  • the inventive composition A1 provides a cured product that fulfills all the requirements of a single-component encapsulation system for high temperature stable insulations: T g > 180 Ā°C, SCT ā‡ -200 Ā°C, CTE ā‡ 20 ppm/K, free of R42 label. Furthermore, the viscosity of the curable composition is sufficient low for applications as encapsulation system for printed circuit boards.
  • the product obtained from Comparative Example C1 has a quite low, but yet insufficient SCT of -131 at a T g of 105Ā°C (which is far too low) and a CTE of 25.7 (which is too high).

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Description

    FIELD OF INVENTION
  • The present invention relates to a curable composition comprising an epoxy resin and a filler composition, a cured product obtained by curing said curable composition as well as the use of the curable composition as insulating material for electrical and electronic components, in particular as encapsulation system for printed circuit boards.
  • So far, the application temperature of encapsulated printed circuit boards used for power electronic applications has been moderate, because the control unit (based on a PCB encapsulated in an organic resin) and the power unit (insulated by ceramic) usually are separated. Thus, a strong heating of the control unit (that needs encapsulation) is avoided and lower grade materials can be used. However, due to the development of new high temperature stable boards based on new thermal stable materials, it will be possible in future to combine both units on a high temperature stable board. Accordingly, in certain applications the encapsulation material needs to withstand high temperatures.
    Customary encapsulating materials are often based on epoxy resins in combination with anhydride hardeners. Some anhydrides, however, have been classified as "respiratory sensitizers" (hazard label: R42) according to REACH legislation.
  • BACKGROUND OF THE INVENTION
  • Accordingly, there is a need for a single-component encapsulation system free from respiratory sensitizer components with high storage stability at ambient temperature, good flow ability at application temperature and which after curing provides a material having high glass transition temperature (Tg > 180 Ā°C) in combination with good long-term thermal aging stability (grade H according to IEC 60216), low coefficient of linear thermal expansion (CTE < 24 ppm/K) and a very good thermal cycle crack resistance (SCT < -200 Ā°C).
  • EP 2 868 692 A1 is directed to a stabilized matrix-filled liquid radiation curable resin composition for additive fabrication including a cationically polymerizable component that is an aliphatic epoxide, a multifunctional (meth)acrylate component, a cationic photoinitiator, a free-radical photoinitiator, and a matrix of inorganic fillers, wherein the matrix constitutes prescribed ratios of at least one microparticle constituent and at least one nanoparticle constituent.
  • It has now been found that a composition containing a cationically polymerisable epoxy resin in combination with a specific filler mixture fulfils the above-mentioned requirements to a great extent.
  • DETAILED DESCRIPTION
  • Accordingly, the invention relates to a composition comprising
    1. (a) a cationically polymerisable epoxy resin,
    2. (b) an initiator for the cationic polymerisation,
    3. (c) a microparticle filler, and
    4. (d) a nanoparticle filler
    according to claim 1.
  • For the preparation of the compositions according to the invention, epoxy resins suitable as component (a) are those customary in epoxy resin technology. Examples of epoxy resins are:
    1. I) Polyglycidyl and poly(Ī²-methylglycidyl) esters, obtainable by reaction of a compound having at least two carboxyl groups in the molecule with epichlorohydrin and Ī²-methylepichlorohydrin, respectively. The reaction is advantageously performed in the presence of bases.
      Aliphatic polycarboxylic acids may be used as the compound having at least two carboxyl groups in the molecule. Examples of such polycarboxylic acids are oxalic acid, succinic acid, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid or dimerised or trimerised linoleic acid.
      It is also possible, however, to use cycloaliphatic polycarboxylic acids, for example hexahydrophthalic acid or 4-methylhexahydrophthalic acid.
      Aromatic polycarboxylic acids, for example phthalic acid, isophthalic acid or terephthalic acid, may also be used as well as partly hydrogenated aromatic polycarboxylic acids such as tetrahydrophthalic acid or 4-methyltetrahydrophthalic acid.
    2. II) Polyglycidyl or poly(Ī²-methylglycidyl) ethers, obtainable by reaction of a compound having at least two free alcoholic hydroxy groups and/or phenolic hydroxy groups with epichlorohydrin or Ī²-methylepichlorohydrin under alkaline conditions or in the presence of an acid catalyst with subsequent alkali treatment.
      The glycidyl ethers of this kind are derived, for example, from acyclic alcohols, e.g. from ethylene glycol, diethylene glycol or higher poly(oxyethylene) glycols, propane-1,2-diol or poly(oxypropylene) glycols, propane-1,3-diol, butane-1,4-diol, poly(oxytetramethylene) glycols, pentane-1,5-diol, hexane-1,6-diol, hexane-2,4,6-triol, glycerol, 1,1,1-trimethylolpropane, pentaerythritol, sorbitol, and also from polyepichlorohydrins.
      Further glycidyl ethers of this kind are derived from cycloaliphatic alcohols, such as 1,4-cyclohexanedimethanol, bis(4-hydroxycyclohexyl) methane or 2,2-bis(4-hydroxycyclohexyl)propane, or from alcohols that contain aromatic groups and/or further functional groups, such as N,N-bis(2-hydroxyethyl)aniline or p,p'-bis(2-hydroxyethylamino)diphenylmethane. The glycidyl ethers can also be based on mononuclear phenols, for example resorcinol or hydroquinone, or on polynuclear phenols, for example bis(4-hydroxyphenyl)methane, 4,4'-dihydroxybiphenyl, bis(4-hydroxyphenyl)sulfone, 1,1,2,2-tetrakis(4-hydroxyphenyl)ethane, 2,2-bis(4-hydroxyphenyl)propane or 2,2-bis(3,5-dibromo-4-hydroxyphenyl) propane.
      Further hydroxy compounds that are suitable for the preparation of glycidyl ethers are novolaks, obtainable by condensation of aldehydes, such as formaldehyde, acetaldehyde, chloral or furfuraldehyde, with phenols or bisphenols that are unsubstituted or substituted by chlorine atoms or by C1-C9alkyl groups, e.g. phenol, 4-chlorophenol, 2-methylphenol or 4-tert-butylphenol.
    3. III) Poly(N-glycidyl) compounds, obtainable by dehydrochlorination of the reaction products of epichlorohydrin with amines containing at least two amine hydrogen atoms. Such amines are, for example, aniline, n-butylamine, bis(4-aminophenyl)methane, m-xylylenediamine or bis(4-methylaminophenyl)methane.
      The poly(N-glycidyl) compounds also include, however, triglycidyl isocyanurate, N,N'-diglycidyl derivatives of cycloalkyleneureas, such as ethyleneurea or 1,3-propyleneurea, and diglycidyl derivatives of hydantoins, such as of 5,5-dimethylhydantoin.
    4. IV) Poly(S-glycidyl) compounds, for example di-S-glycidyl derivatives, derived from dithiols, e.g. ethane-1,2-dithiol or bis(4-mercaptomethylphenyl)ether.
    5. V) Cycloaliphatic epoxy resins, e.g. bis(2,3-epoxycyclopentyl)ether, 2,3-epoxycyclopentylglycidyl ether, 1,2-bis(2,3-epoxycyclopentyloxy) ethane or 3,4-epoxycyclohexylmethyl-3',4'-epoxycyclohexanecarboxylate.
  • It is also possible, however, to use epoxy resins wherein the 1,2-epoxy groups are bonded to different hetero atoms or functional groups; such compounds include, for example, the N,N,O-triglycidyl derivative of 4-aminophenol, the glycidyl ether glycidyl ester of salicylic acid, N-glycidyl-N'-(2-glycidyloxypropyl)-5,5-dimethylhydantoin and 2-glycidyloxy-1,3-bis(5,5-dimethyl-l-glycidylhydantoin-3-yl)propane.
  • Preferably component (a) is a cycloaliphatic epoxy resin.
  • The term "cycloaliphatic epoxy resin" in the context of this invention denotes any epoxy resin having cycloaliphatic structural units, that is to say it includes both cycloaliphatic glycidyl compounds and Ī²-methylglycidyl compounds as well as epoxy resins based on cycloalkylene oxides.
  • Suitable cycloaliphatic glycidyl compounds and Ī²-methylglycidyl compounds are the glycidyl esters and Ī²-methylglycidyl esters of cycloaliphatic polycarboxylic acids, such as tetrahydrophthalic acid, 4-methyltetrahydrophthalic acid, hexahydrophthalic acid, 3-methylhexahydrophthalic acid and 4-methylhexahydrophthalic acid.
  • Further suitable cycloaliphatic epoxy resins are the diglycidyl ethers and Ī²-methylglycidyl ethers of cycloaliphatic alcohols, such as 1,2-dihydroxycyclohexane, 1,3-dihydroxycyclohexane and 1,4-dihydroxycyclohexane, 1,4-cyclohexanedimethanol, 1,1-bis(hydroxymethyl) cyclohex-3-ene, bis(4-hydroxycyclohexyl)methane, 2,2-bis(4-hydroxycyclohexyl)propane and bis(4-hydroxycyclohexyl)sulfone.
  • Examples of epoxy resins having cycloalkylene oxide structures are bis(2,3-epoxycyclopentyl)ether, 2,3-epoxycyclopentylglycidyl ether, 1,2-bis(2,3-epoxycyclopentyl)ethane, vinyl cyclohexene dioxide, 3,4-epoxycyclohexylmethyl 3',4'-epoxycyclohexanecarboxylate, 3,4-epoxy-6-methylcyclohexylmethyl-3 ',4'-epoxy-6'-methylcyclohexanecarboxylate, bis(3,4-epoxycyclohexylmethyl)adipate and bis(3,4-epoxy-6-methylcyclohexylmethyl)adipate.
  • In a further preferred embodiment the composition according to the invention contains as component (a) a cycloaliphatic epoxy resin selected from bis(4-hydroxycyclohexyl)methane-diglycidyl ether, 2,2-bis(4-hydroxycyclohexyl)propanediglycidyl ether, tetrahydrophthalic acid diglycidyl ester, 4-methyltetrahydrophthalic acid diglycidyl ester, 4-methylhexahydrophthalic acid diglycidyl ester and, in particular, 3,4-epoxycyclohexylmethyl3',4'-epoxycyclohexanecarboxylate.
  • As initiator system for the cationic polymerisation of the epoxy resin there is used
    a mixture comprising
    • (b1) a quaternary ammonium salt with an aromatic heterocyclic cation having one or two nitrogen atoms and a non-nucleophilic anion selected from BF4 -, PF6 -, SbF6 -, SbF5OH-, BXpYq - or CF3(CF2)mSO3 -, wherein p and q are 0, 1, 2, 3 or 4, provided that p + q = 4, X denotes halogen or hydroxyl,
      Y represents phenyl or naphthyl which are unsubstituted or substituted by fluoro, trifluoromethyl, trifluoromethoxy, nitro or cyano,
      m is 0 or an integer from 1 to 17, and
    • (b2) a compound of formula (5)
      Figure imgb0001
      wherein R8, R9, R10 and R11 independently of the other are phenyl that is unsubstituted or substituted by C1-C12alkyl, C1-C12alkoxy, C7-C36aralkyl, C6-C36aryl, C3-C15alkoxyalkyl, C1-C12alkylthio, C1-C12alkylcarbonyl, halogen, nitro or cyano, and
      R12 and R13 independently of the other are hydrogen or C1-C12alkyl.
  • Preferably the compositions according to the invention contain as component (b1) a quaternary ammonium salt with an aromatic heterocyclic cation of formula (1), (2) or (3)
    Figure imgb0002
    wherein R1 is C1-C12alkyl, C7-C36aralkyl, C3-C15alkoxyalkyl or benzoylmethyl, R2, R3, R4 , R5 and R6 independently of the other are hydrogen, C1-C4alkyl or phenyl or R2 and R3 or R3 and R4 or R4 and R5 or R5 and R6 together with the carbon atoms to which they are attached form a benzene, naphthalene, pyridine or quinoline ring.
  • When any of the radicals R1 - R6 is alkyl, that radical or those radicals may be straight-chain or branched. Examples of alkyl groups are methyl, ethyl, n-propyl, isopropyl, n-butyl, isobutyl, sec-butyl, tert-butyl, n-pentyl, neopentyl, n-hexyl, n-heptyl, n-octyl, isooctyl, n-decyl and n-dodecyl.
  • Aralkyl groups as R1 have preferably from 7 to 30 carbon atoms, especially from 7 to 12 carbon atoms.
  • Examples of suitable aralkyl groups are benzyl, 2-phenylethyl, tolylmethyl, mesitylmethyl and 4-chlorophenylmethyl.
  • Examples of suitable alkoxyalkyl groups are 2-methoxyethyl, 3-methoxypropyl, 4-methoxybutyl, 6-methoxyhexyl, 2-ethoxyethyl, 3-ethoxypropyl, 4-ethoxybutyl and 6-methoxyhexyl.
  • More preferably, the composiztions contain as component (b1) a quaternary ammonium salt of formula (4)
    Figure imgb0003
    wherein R7 denotes methyl, ethyl, n-butyl, benzyl or benzoylmethyl, and Z- is hexafluorophosphate, hexafluoroarsenate, hexafluoroantimonate, pentafluorohydroxyantimonate, tetrafluoroborate, tetrakis[3,5-bis(trifluoromethyl)-phenyl]borate and tetrakis(pentafluorophenyl)borate.
  • Individual examples of suitable compounds of the formula (4) are N-methylquinolinium hexafluorophosphate, N-methylquinolinium hexafluoroarsenate, N-methylquinolinium hexafluoroantimonate, N-methylquinolinium pentafluorohydroxyantimonate, N-methylquinolinium tetrafluoroborate, N-methylquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate, N-methylquinolinium tetrakis(pentafluorophenyl)borate, N-ethylquinolinium hexafluorophosphate, N-ethylquinolinium hexafluoroarsenate, N-ethylquinolinium hexafluoroantimonate, N-ethylquinolinium pentafluorohydroxyantimonate, N-ethylquinolinium tetrafluoroborate, N-ethylquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate, N-ethylquinolinium tetrakis(pentafluorophenyl)borate, N-butylquinolinium hexafluorophosphate, N-butylquinolinium hexafluoroarsenate, N-butylquinolinium hexafluoroantimonate, N-butylquinolinium pentafluorohydroxyantimonate, N-butylquinolinium tetrafluoroborate, N-butylquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate, N-butylquinolinium tetrakis(pentafluorophenyl)borate, N-benzylquinolinium hexafluorophosphate, N-benzylquinolinium hexafluoroarsenate, N-benzylquinolinium hexafluoroantimonate, N-benzylquinolinium pentafluorohydroxyantimonate, N-benzylquinolinium tetrafluoroborate, N-benzylquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate, N-benzylquinolinium tetrakis(pentafluorophenyl)borate, N-benzoylmethyquinolinium hexafluorophosphate, N-benzoylmethyquinolinium hexafluoroarsenate, N-benzoylmethyquinolinium hexafluoroantimonate, N-benzoylmethyquinolinium pentafluorohydroxyantimonate, N-benzoylmethyquinolinium tetrafluoroborate, N-benzoylmethyquinolinium tetrakis[3,5-bis(trifluoromethyl)phenyl]borate and N-benzoylmethyquinolinium tetraki s(pentafluorophenyl)borate.
  • The most preferred compound of the formula (4) is N-benzylquinolinium hexafluoroantimonate.
  • As mentioned hereinabove, (b2) is a compound of formula (5)
    Figure imgb0004
    wherein R8, R9, R10 and R11 independently of the other are phenyl that is unsubstituted or substituted by C1-C12alkyl, C1-C12alkoxy, C7-C36aralkyl, C6-C36aryl, C3-C15alkoxyalkyl, C1-C12alkylthio, C1-C12alkylcarbonyl, halogen, nitro or cyano, and
    R12 and R13 independently of the other are hydrogen or C1-C12alkyl.
  • Examples for suitable compounds of formula (5) are 1,2-bis(2-methylphenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2-ethylphenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2-fluorophenyl)-1,2-diphenyl-1,2-ethanediol, 1,2-bis(2,6-difluorophenyl)-1,2-diphenyl-1,2-ethanediol and, in particular, 1,1,2,2-tetraphenyl-1,2-ethanediol.
  • The compositions according to the invention optionally comprise a curing accelerator as additional component. Suitable accelerators are known to the person skilled in the art. Examples that may be mentioned are:
    • complexes of amines, especially tertiary amines, with boron trichloride or boron trifluoride; tertiary amines, such as benzyldimethylamine;
    • urea derivatives, such as N-4-chlorophenyl-N',N'-dimethylurea (monuron) ; unsubstituted or substituted imidazoles, such as imidazole or 2-phenylimidazole.
  • Preferred accelerators are imidazoles, in particular N-methylimidazole.
  • An essential component of the curable composition according to the present invention is a filler composition comprising a microparticle filler and a nanoparticle filler.
  • The microparticle filler is preferably selected from globular or angular metal or semi-metal oxides, nitrides, carbides and hydroxides, especially from the goup consisting of silica flour, amorphous silica (natural amorphous silica or fused silica), aluminium oxide, silicon carbide, boron nitride, aluminium nitride, aluminium hydroxide and magnesium hydroxide.
  • According to a preferred embodiment the microparticles have an average particle size (d50) of 1 to 100 Āµm, more preferably from 2 to 50 Āµm and most preferably from 5 to 25 Āµm determined according to ISO 13320-1:1999.
  • Component (c) of the compositions according to the invention is preferably amorphous silica. Advantageously, the amorphous silica is natural amorphous silica or fused silica. Fused silica with an average particle size (d50) of 10.5 Āµm is commercially available under the name TECOSILĀ® from CE Minerals, Greenville, TN, USA. Natural amorphous silica is available under the name AMOSILĀ® from Quarzwerke, Germany.
  • According to a preferred embodiment the amorphous silica has an average particle size d50 of 1 to 100 Āµm, more preferably from 2 to 50 Āµm and most preferably from 5 to 25 Āµm determined according to ISO 13320-1:1999.
  • In a further preferred embodiment the amorphous silica is surface treated. Preferably, the amorphous silica is surface treated with a silane, more preferably selected from the group consisting of amino silane, epoxy silane, (meth)acrylic silane, methyl silane and vinyl silane.
  • Preferably the silane is a compound of the following formula:
    Figure imgb0005
    wherein R denotes methyl or ethyl.
  • The nanoparticle fillers are preferably selected from oxides, carbonates, nitrides and silicates of magnesium, calcium, boron, aluminium and silicon.
  • Especially preferred nanoparticle fillers essentially consist of calcium carbonate, boron nitride, montmorillonite or silicon dioxide.
  • Silica nanoparticles are particularly preferred.
  • The preparation of silicon dioxide nanoparticles is disclosed, for example, in WO 02/083776 . The preferred silicon dixide nanoparticles are substantially spherical and have only slight, if any, agglomeration and/or aggregation. The nanoparticles are preferably surface-modified in order to prevent or reduce their agglomeration. In the case of silicon dioxide, a preferred surface modification is silanization with appropriate silanes, for examples the silanes mentioned above as surface modification agents for silica microparticles.
  • Such nanoparticle fillers are known and to some extent commercially available, for example under the designation NANOPOXĀ® (supplied by Evonik). A preferred nanopartikel filler is NANOPOXĀ® E 601, which is a dispersion of silica nanoparticles in a cycloaliphatic epoxy resin.
  • The average particle size of the silica nanoparticles d50 is usually between 2 and 100 nm, preferably between 6 and 40 nm, more preferably between 8 and 80 nm and in particular between 10 and 25 nm.
    D50 is known as the medium value of particle diameter. This means that a powder comprises 50% of particles having a larger particle size and 50% of particles having a smaller particle size than the dso value.
  • The relative amounts of components (a), (b), (c) and (d) may vary within wide ranges. Preferably, the total amount of filler (c) + (d) is 60 to 90 % by weight, preferably 65 to 85 % by weight and in particular 70 - 80 % by weight based on the total composition (a) + (b) + (c) + (d).
  • Preferably, the amount of microparticle filler (c) is 55 to 80 % by weight, more preferably 60 to 75 % by weight and in particular 65 to 70 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • Preferably, the amount of nanoparticle filler (d) is 2 to 20 % by weight, more preferably 5 to 15 % by weight and in particular 7 to 12 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • The amount of cationically polymerisable epoxy resin (a) is preferably 10 to 40 % by weight, more preferably 15 to 30 % by weight and in particular 20 to 25 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • The amount of initiator for the cationic polymerisation initiator (b) is preferably 0.05 to 1.0 % by weight, more preferably 0.1 to 0.7 % by weight and in particular 0.2 to 0.5 % by weight. based on the total composition (a) + (b) + (c) + (d).
  • The curable composition according to the present invention can additionally comprise further additives, such as flexibilizers, thixotropic agents, wetting agents, antisettling agents, colour agents, defoamers, light stabilizers, mold release agents, toughening agents, adhesion promoters, flame retardants, curing accelerators, etc.
  • The compositions according to the present invention are heat-curable mixtures.
    To carry out the curing reaction, the cationically polymerisable epoxy resin (a) is mixed with the required amount of the initiator for the cationic polymerisation (b). These mixtures are stable at room temperature and can be handled without hazard. In general, it is not necessary to add any additional activating component prior to initiation of polymerisation, so that the mixtures are one-component systems which can be cured at any time. The polymerisation is initiated by heating the the mixture to temperatures of 60 - 220 Ā°C, preferably 80 - 200 Ā°C and in particular 100 .- 190 Ā°C, depending on the material used and the desired polymerisation time.
  • The cured products demonstrate surprisingly excellent mechanical properties, in particular with respect to thermal stability and crack resistance.
  • Therefore, a further embodiment of the present invention is a cured product which is obtainable by curing a curable composition according to the present invention.
  • The cured products according to the present invention are preferably used as electrically insulating construction material for electrical or electronic components.
  • The curable compositions according to the invention can specifically be applied as casting system for medium to high voltage applications, e.g for insulators, bushings, transformers, instrument transformers and switchgears, in all cases for indoor as well as outdoor applications, especially as encapsulation systems for printed circuit boards.
    The curable compositions according to the invention may be used as encapsulation material for stators and rotors of electrical machines such as motors or generators. They may be used either as full encapsulation systems or only for impregnation of the end turns of the windings.
  • Accordingly, a further embodiment of the present invention is a method for the manufacturing of electrical insulation equipment comprising the steps:
    1. (i) applying a curable composition according to the present invention to the housing of electrical components; and
    2. (ii) curing the curable composition at a temperature > 60 Ā°C.
  • The invention further relates to the use of the composition according to the invention as insulating material for electrical and electronic components.
  • Preferably, the composition according to the invention is used as encapsulation system for printed circuit boards.
  • A further embodiment of the present invention is the use of the curable compositions as adhesives.
  • The invention is illustrated by the following non-limiting examples.
  • Examples Measurement of properties:
  • Unless otherwise indicated, the viscosity is determined with a Rheomat equipment (type 115, MS DIN 125 D = 10/s) at 60Ā°C
    Tensile strength and elongation at break are determined at 23 Ā°C according to ISO R527 KIC (critical stress intensity factor) in MPa ā€¢ m
    Figure imgb0006
    and GIC (specific break energy) in J/m2 are determined at 23 Ā°C by double torsion experiment (Huntsman-internal method).
    CTE (coefficient of linear thermal expansion) is determined according to DIN 53752
    Tg (glass transition temperature) is determined according to ISO 6721/94
    SCT: Crack index (simulated crack temperature) is calculated based on Tg, GIC, CTE and elongation at break according to the description given in WO 00/55254 .
  • List of used raw materials
  • ARALDITEĀ®CY 179-1:
    3,4-epoxycyclohexyl)methyl 3,4-epoxycyclohexanecarboxylate (supplied by Huntsman Advanced Materials (Switzerland) GmbH)
    ARALDITEĀ® XB 5992
    liquid, low viscous bisphenol A epoxy resin, epoxide number: 4.9 - 5.1 eq/kg (supplied by Huntsman)
    ARALDITEĀ® XB 5993
    liquid, pre-accelerated anhydride curing agent. (supplied by Huntsman)
    ARADURĀ® HY 906
    anhydride curing agent, mixture of 1-methyl-5-norbomene-2,3-dicarboxylic anhydride and 5-norbornene-2,3-dicarboxylic anhydride (supplied by Huntsman)
    ACCELERATOR 1:
    1-methylimidazole
    INITIATOR 1:
    N-benzylquinolinium hexafluoroantimonate (supplied by Huntsman)
    CO-INITIATOR 1:
    1,1,2,2-tetraphenyl-1,2-ethanediol (supplied by Natland Int. Corp.)
    NANOPOXĀ® E 601:
    60 % by weight of 3,4-epoxycyclohexyl)methyl-3,4-epoxycyclohexanecarboxylate and 40 % by weight of surface-modified silica nanoparticles (supplied by Evonik)
    AEROSILĀ® R 972:
    (supplied by Evonik) fumed silica aftertreated with DDS (Dimethyldichlorosilane),
    AMOSILĀ® 510 :
    (supplied by Quarzwerke) fused silica produced from natural amorphous silica by grinding with subsequent air separation; average particle size d50: 11 Āµm (supplied by Quarzwerke)
    AMOSILĀ® 520:
    fused silica produced from natural amorphous silica by grinding with subsequent air separation; average particle size d50: 21 Āµm (supplied by Quarzwerke)
    BYK W 940
    anti-settling additive (supplied by: BYK-Chemie GmbH),
    BYK W 995
    wetting and dispersing agent, phosphate-containing polyester (supplied by: BYK-Chemie GmbH),
    BYK 070:
    defoaming agent based on silicones and polymers (supplied by: BYK-Chemie GmbH)
    SILFOAMĀ® SH:
    antifoam agent, (supplied by Wacker)
    BAYFERROXĀ® 225
    iron oxide pigment (supplied by Lanxess)
    TREMINĀ® 283-600
    wollastonite, surface-treated with a epoxysilane, average particle size d50: 21 Āµm (supplied by Quarzwerke)
    SILAN A-187
    Ī³-glycidyloxypropyltrimethoxysilane (supplied by Momentive)
    Example A1
  • Initially, 2 master batches containing the ingredients of the initiator are prepared as follows:
    • Masterbatch A: 90 g of ARALDITEĀ® CY 179-1 and 10 g of Co-initiator 1 are mixed at 90 Ā°C for 30 min. The resulting clear solution is cooled to room temperature (RT).
    • Masterbatch B: 90 g of ARALDITEĀ® CY 179-1 and 10 g of Initiator 1 are mixed at 60 Ā°C for 30 min. The resulting clear solution is cooled to RT.
    138 g of ARALDITEĀ® CY 179-1, 450 g of NANOPOXĀ® E 601, 34 g of Master batch A, 26 g of Master batch B, 4.2 g of SILFOAMĀ® SH, 10 g BYK-W 940, 4.2 g BYK 070 and 4.0 g AEROSILĀ® R 972 are put into an Esco mixer of sufficient size. The content of the mixer is then stirred with a disperser stirrer with 100 rpm while heating up to 50 Ā°C.
    Then 435 g of AMOSILĀ® 510 and 894.6 g of AMOSILĀ® 520 are added slowly in several portions while mixing at 100 rpm. After 5 min the mixer is stopped and the walls are scratched and the material is put into the mixture. Then the mixture is stirred for another 70 min. under vacuum at 50 Ā°C. After 30 min. of mixing the walls are scratched again and the material is put into the mixture.
    To produce 4 mm thick test plates, metal molds were preheated to about 80 Ā°C in an oven. Then the degassed resin is poured in the mold. The mold is then put to an oven at 120 Ā°C for 1 hour. After that the oven temperature is raised to 180 Ā°C for 90 min. Then the mold is taken out of the oven and opened after cooling down to room temperature. The obtained plate is used to cut out test specimens for the K1C/ G1C tests, for the tensile strength testing, the Tg measurement via DSC and the determination of the CTE according to the standards mentioned above. The results are given in Table 1. Comparative Example C1
  • As described in Example 2 of WO 2010/112272 , 100 g of ARALDITEĀ® XB 5992 are mixed with 90 g of ARALDITE XB 5993 and the mixture is heated while slightly stirring with a propeller stirrer to about 60 Ā°C for about 5 minutes. Then the mixer is stopped and 2 g of BAYFERROXĀ® 225 is added and the mixer is started again for about 1 min. Subsequently, while stirring, 51.3 g of TREMINĀ® 283-600 EST and 290.7 g of AMOSILĀ® 520 are added in portions and the mixture is heated up to 60 Ā°C under stirring for about 10 minutes. Then the mixer is stopped and the vessel is degassed carefully by applying a vacuum for about 1 minute.
    The mixture is poured into a 140 Ā°C hot steel mold to prepare plates for the determination of the properties (4 mm thickness). The mold is then put to an oven for 30 minutes at 140Ā°C. After thermally curing the mold, the mold is taken out of the oven and the plates are cooled down to ambient temperature (25Ā°C).
    The results of the tests are summarised in Table 1.
  • Comparative Example C2 1. Epoxy resin formulation:
  • 950 g NANOPOXĀ® E 601, 3.75 g SILFOAMĀ® SH, 5.0 g BYK W 955, 6.25 g BYK 070, 12.5 g SILAN A-187 and 22.5 g AEROSILĀ® R 972 are put to a Esco mixer of sufficient size. The content of the mixer is then heated up 60 Ā°C and stirred with a dissolver stirrer with 300 rpm under vacuum at 60 Ā°C for 3 min. Then the vacuum is broken and 500 g of AMOSILĀ® 510 and 1000 g of AMOSILĀ® 520 are added slowly in several portions while mixing at 300 rpm at 60 - 65 Ā°C under vacuum. After 10 min the mixer is stopped, the vacuum is broken and the walls are scratched and the material is put to the mixture. Then the mixture is stirred another 5 min. under vacuum at 60-65 Ā°C. The vacuum is broken and the mixer walls are scratched again. Finally the mixture is stirred for 20 min. under vacuum at 300 rpm at 60- 65 Ā°C
  • 2. Hardener formulation:
  • 879.8 g ARADURĀ®HY 906, 7.4 g ACCELERATOR 1, 10 g SILAN A-187 and 10 g of BYK-W 940 are put to an Esco mixer of sufficient size. The content of the mixer is then heated up 50 Ā°C and stirred with a dissolver stirrer with 300 rpm under vacuum at 50 Ā°C for 3 min. Then the vacuum is broken and 1092.8 g of AMOSILĀ® 510 are added slowly in several portions while mixing at 300 rpm at 50 Ā°C under vacuum. After 10 min the mixer is stopped, the vacuum is broken and the walls are scratched and the material is put to the mixture. Then the mixture is stirred another 5 min. under vacuum at 50-55 Ā°C. The vacuum is broken and the mixer walls are scratched again. Finally the mixture was stirred for 20 min. under vacuum at 300 rpm at 55-60 Ā°C.
  • 3. Preparation of resin/hardener-mixture and curing:
  • 500 g of resin formulation and 325 g of hardener formulation are put together and heated to about 60 Ā°C while stirring with 100 rpm under vacuum.
    To produce 4 mm thick test plates, metal molds are preheated to about 80 Ā°C in an oven. Then the degassed resin/hardener mixture is poured into the mold. The mold is then put to an oven at 100 Ā°C for one hour, then for 1.5 hours at 140 Ā°C and finally for 1.5 hours at 210 Ā°C. Then the mold is taken out of the oven and opened after cooling down to room temperature. The cured plate is subjected to various tests the results of which are given in Table 1. Table 1: The amounts of the ingredients of Compositions A1, C1 and C2 are given in parts by weight
    Composition A1 C1 C2
    ARALDITEĀ® CY 179-1 9.60
    ARALDITEĀ® XB 5992 18.73
    INITIATOR 1 0.13
    CO-INITIATOR 1 0.17
    ARALDITEĀ® XB 5993 16.85
    ARADURĀ® HY 906 17.33
    ACCELERATOR 1 0.15
    NANOPOXĀ® E 601 22.50 23.03
    AEROSILĀ® R 972 0.20 0.55
    AMOSILĀ® 510 21.75 33.65
    AMOSILĀ® 520 44.73 54.44 24.24
    TREMINĀ® 283-600 9.61
    BYK W 940 0.50 0.20
    BYK W 995 0.12
    BYK 070 0.21 0.15
    SILFOAMĀ® SH 0.21 0.09
    SILAN A-187 0.50
    BAYFERROXĀ® 225 0.37
    Viscosity at 60 Ā°C/PaĀ·s 15 8.6 5
    Curing conditions 1h/120 Ā°C 30 min/140 Ā°C 1 h/100 Ā°C
    1.5 h/180 Ā°C 1.5 h/140 Ā°C
    1.5 h/210 Ā°C
    Tensile strength/MPa 75 86 62.3
    Elongation at break/% 0.6 1.1 0.65
    K 1 C / MPa ā‹… āˆš m
    Figure imgb0007
    2.4 2.4 2.2
    G1C/J/m2 320 441 362
    R42 lable no yes yes
    CTE/ppm/K 20 25.7 24
    Tg/Ā°C 184 105 205
    SCT/Ā°C -271 -131 -184
  • Discussion of Test Results
  • The inventive composition A1 provides a cured product that fulfills all the requirements of a single-component encapsulation system for high temperature stable insulations:
    Tg > 180 Ā°C, SCT < -200 Ā°C, CTE < 20 ppm/K, free of R42 label.
    Furthermore, the viscosity of the curable composition is sufficient low for applications as encapsulation system for printed circuit boards.
    The product obtained from Comparative Example C1 has a quite low, but yet insufficient SCT of -131 at a Tg of 105Ā°C (which is far too low) and a CTE of 25.7 (which is too high). The properties of the cured product according to Comparative Example C2 are satisfactory with respect to Tg and CTE, but completely insufficient with respect to SCT. It is not a solution to the problem because it is R42-labelled, but mainly because the SCT is far too high (-84 Ā°C vs. target of -200 Ā°C). Furthermore, Composition C2 suffers from the classification as hazardous substance (label R42, "respiratory sensitizer")

Claims (12)

  1. A composition comprising
    (a) a cationically polymerisable epoxy resin,
    (b) an initiator for the cationic polymerisation,
    (c) a microparticle filler, and
    (d) a nanoparticle filler
    wherein component (b) is a mixture comprising
    (b1) a quaternary ammonium salt with an aromatic heterocyclic cation having one or two nitrogen atoms and a non-nucleophilic anion selected from BF4 -, PF6 -, SbF6 -, SbF5OH-, BXpYq - or CF3(CF2)mSO3 -, wherein p and q are 0, 1, 2, 3 or 4, provided that p + q = 4, X denotes halogen or hydroxyl,
    Y represents phenyl or naphthyl which are unsubstituted or substituted by fluoro, trifluoromethyl, trifluoromethoxy, nitro or cyano,
    m is 0 or an integer from 1 to 17, and
    (b2) a compound of formula (5)
    Figure imgb0008
    wherein R8, R9, R10 and R11 independently of the other are phenyl that is unsubstituted or substituted by C1-C12alkyl, C1-C12alkoxy, C7-C36aralkyl, C6-C36aryl, C3-C15alkoxyalkyl, C1-C12alkylthio, C1-C12alkylcarbonyl, halogen, nitro or cyano, and
    R12 and R13 independently of the other are hydrogen or C1-C12alkyl.
  2. The composition according to claim 1 containing a cycloaliphatic epoxy resin as component (a).
  3. The composition according to claim 2 containing as component (a) a cycloaliphatic epoxy resin selected from bis(4-hydroxycyclohexyl)methanediglycidyl ether, 2,2-bis(4-hydroxycyclohexyl)propanediglycidyl ether, tetrahydrophthalic acid diglycidyl ester, 4-methyltetrahydrophthalic acid diglycidyl ester, 4-methylhexahydrophthalic acid diglycidyl ester and 3,4-epoxycyclohexylmethyl 3',4'-epoxycyclohexanecarboxylate.
  4. The composition according to any of claims 1 - 3 containing as component (b1) a quaternary ammonium salt with an aromatic heterocyclic cation of formula (1), (2) or (3)
    Figure imgb0009
    wherein R1 is C1-C12alkyl, C7-C36aralkyl, C3-C15alkoxyalkyl or benzoylmethyl, R2, R3, R4 , R5 and R6 independently of the other are hydrogen, C1-C4alkyl or phenyl or R2 and R3 or R3 and R4 or R4 and R5 or R5 and R6 together with the carbon atoms to which they are attached form a benzene, naphthalene, pyridine or quinoline ring.
  5. The composition according to claim 4 containing as component (b1) a quaternary ammonium salt of formula (4)
    Figure imgb0010
    wherein R7 denotes methyl, ethyl, n-butyl, benzyl or benzoylmethyl, and
    Z- is hexafluorophosphate, hexafluoroarsenate, hexafluoroantimonate, pentafluorohydroxyantimonate, tetrafluoroborate, tetrakis[3,5-bis(trifluoromethyl)-phenyl]borate and tetrakis(pentafluorophenyl)borate.
  6. The composition according to any of claims 1 - 5, containing as component (c) amorphous silica.
  7. The composition according to any of claims 1 - 6, containing as component (d) silica nanoparticles.
  8. The composition according to any of claims 1 - 7 wherein the total amount of filler (c) + (d) is 60 to 90 % by weight, based on the total composition (a) + (b) + (c) + (d).
  9. The composition according to any of claims 1 - 8 wherein the amount of nanoparticle filler (d) is 2 to 20 % by weight, based on the total composition (a) + (b) + (c) + (d).
  10. A method for the manufacturing of electrical insulation equipment comprising the steps
    (i) applying a curable composition according to any of claims 1 - 9 to the housing of electrical
    components; and
    (ii) curing the curable composition.at a temperature > 60 Ā°C.
  11. The cured product obtainable by curing a curable composition according to any of claims 1 to 9.
  12. The use of the composition according to any of claims 1 - 9 as insulating material for electrical and electronic components or as encapsulation material for stators and rotors of electrical machines such as motors or generators.
EP16730283.5A 2015-06-16 2016-06-03 Epoxy resin composition Active EP3310838B1 (en)

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Families Citing this family (8)

* Cited by examiner, ā€  Cited by third party
Publication number Priority date Publication date Assignee Title
EP3460809A1 (en) * 2017-09-20 2019-03-27 Siemens Aktiengesellschaft Electrical insulation material and/or impregnating resin for roll tape insulation of a medium and/or high voltage machine, insulation material and insulation system
JP6516115B1 (en) * 2018-05-16 2019-05-22 å±±ę „åŒ–å­¦ę Ŗ式会ē¤¾ Soluble and non-soluble particle-containing curable resin composition
FI3953408T3 (en) * 2019-04-11 2023-08-21 Huntsman Adv Mat Licensing Switzerland Gmbh Curable two-component resin-based system
CN114242318A (en) * 2019-06-20 2022-03-25 å¹æč„æēŗµč§ˆēŗæē¼†é›†å›¢ęœ‰é™å…¬åø Heat insulation composite cable
CN114420385A (en) * 2019-06-20 2022-04-29 å¹æč„æēŗµč§ˆēŗæē¼†é›†å›¢ęœ‰é™å…¬åø Preparation process of fire-resistant cable
WO2022030252A1 (en) * 2020-08-07 2022-02-10 ę˜­å’Œé›»å·„ćƒžćƒ†ćƒŖć‚¢ćƒ«ć‚ŗę Ŗ式会ē¤¾ Insulating material for stator, stator, and method for manufacturing stator
EP4267646A1 (en) 2020-12-22 2023-11-01 Huntsman Advanced Materials Licensing (Switzerland) GmbH Curable two-part resin system
WO2024083741A1 (en) 2022-10-18 2024-04-25 Huntsman Advanced Materials Licensing (Switzerland) Gmbh Method to avoid cracks in encapsulation of sharp-edged inserts

Family Cites Families (28)

* Cited by examiner, ā€  Cited by third party
Publication number Priority date Publication date Assignee Title
US4058401A (en) 1974-05-02 1977-11-15 General Electric Company Photocurable compositions containing group via aromatic onium salts
JPS5214654A (en) * 1975-07-24 1977-02-03 Shin Etsu Chem Co Ltd An organopolysiloxane composition
IT1070929B (en) * 1975-11-14 1985-04-02 Carrier Corp ALCOHOL CIRCULATION PLANT
US4336363A (en) 1979-02-12 1982-06-22 General Electric Company Heat curable compositions containing sulfonium salts
US4393185A (en) 1981-06-02 1983-07-12 Ciba-Geigy Corporation Thermally polymerizable mixtures and processes for the thermally-initiated polymerization of cationically polymerizable compounds
ES2045878T3 (en) 1989-01-16 1994-01-16 Ciba Geigy Ag ARALIFATIC SULPHONIUM SALTS AND THEIR USE.
JP3189988B2 (en) * 1992-07-07 2001-07-16 ä½å‹ćƒ™ćƒ¼ć‚Æćƒ©ć‚¤ćƒˆę Ŗ式会ē¤¾ Insulating resin paste
TW237466B (en) 1992-07-21 1995-01-01 Giba Gerigy Ag
ES2134425T3 (en) 1994-03-16 1999-10-01 Ciba Sc Holding Ag SINGLE COMPONENT EPOXY RESIN SYSTEMS FOR THE DRIPPING PROCEDURE AND THE HOT ROTATION IMMERSION PROCEDURE.
ES2193341T3 (en) * 1996-06-17 2003-11-01 Vantico Ag MANUFACTURE OF MOLDED OBJECTS OF A COMPOSITION WITH AN EPOXY RESIN MONOCOMPONENT THROUGH THE AUTOMATIC PRESSURE GELIFICATION TECHNIQUE.
JP2007180044A (en) * 1997-02-03 2007-07-12 Shin Etsu Chem Co Ltd Method of improving high-voltage electrical insulating characteristic of polymer insulator
US6214905B1 (en) * 1997-12-23 2001-04-10 Cookson Singapore Pte Ltd C/O Alpha Metals, Inc. Epoxy mold compound and method
DE69905173T2 (en) 1998-07-15 2003-07-24 Vantico Ag HEAT-CURABLE EPOXY COMPOSITIONS
BR9916010A (en) * 1998-12-09 2001-09-04 Vantico Ag Hydrophobic epoxy resin system
JP3581268B2 (en) * 1999-03-05 2004-10-27 ę Ŗ式会ē¤¾ę±čŠ Semiconductor device with heat sink and method of manufacturing the same
JP4798848B2 (en) 1999-03-16 2011-10-19 ćƒćƒ³ćƒ„ćƒžćƒ³ ć‚¢ćƒ‰ćƒćƒ³ć‚¹ćƒˆ 惞惆ćƒŖć‚¢ćƒ«ć‚ŗ ļ¼ˆć‚¹ć‚¤ćƒƒćƒ„ć‚”ćƒ©ćƒ³ćƒ‰ļ¼‰ ć‚²ćƒ¼ć‚Øćƒ ćƒ™ćƒ¼ćƒćƒ¼ Curable composition having a special combination of properties
US6764616B1 (en) * 1999-11-29 2004-07-20 Huntsman Advanced Materials Americas Inc. Hydrophobic epoxide resin system
EP1236765A1 (en) 2001-02-28 2002-09-04 hanse chemie GmbH Silica dispersion
US20050040562A1 (en) * 2003-08-19 2005-02-24 3D Systems Inc. Nanoparticle-filled stereolithographic resins
CN1938356B (en) * 2004-03-30 2010-11-17 ę Ŗ式会ē¤¾é’ŸåŒ– Hardenable composition
DE602006006338D1 (en) * 2005-11-22 2009-05-28 Huntsman Adv Mat Switzerland WEATHERPROOF EPOXY RESIN SYSTEM
KR100965739B1 (en) * 2006-02-17 2010-06-24 ģ£¼ź³ ź¾ø ė„ė£Œ ź°€ė¶€ģ‹œķ‚¤ź°€ģ“ģƒ¤ Curable organopolysiloxane composition and antifouling composite coating film
JP2008075069A (en) * 2006-08-23 2008-04-03 Toshiba Corp Casting resin composition and insulating material and insulating structure using the same
US8309633B2 (en) * 2008-07-17 2012-11-13 Henkel Ireland Ltd. Low temperature, cationically curable compositions with improved cure speed and toughness
ES2411462T3 (en) * 2009-04-02 2013-07-05 Huntsman Advanced Materials (Switzerland) Gmbh Direct overmolding
JP5615374B2 (en) * 2009-10-21 2014-10-29 ćƒćƒ³ćƒ„ćƒžćƒ³ćƒ»ć‚¢ćƒ‰ćƒ“ć‚”ćƒ³ć‚¹ćƒˆćƒ»ćƒžćƒ†ćƒŖć‚¢ćƒ«ć‚ŗ惻ļ¼ˆć‚¹ć‚¤ćƒƒćƒ„ćƒ©ćƒ³ćƒ‰ļ¼‰ćƒ»ć‚²ćƒ¼ć‚Øćƒ ćƒ™ćƒ¼ćƒćƒ¼ Thermosetting composition
DE102010015398A1 (en) * 2010-04-19 2011-10-20 Siemens Aktiengesellschaft Insulating composite material for electrical insulation, method of making and using same
EP2868692B1 (en) * 2013-11-05 2017-10-25 DSM IP Assets B.V. Stabilized matrix-filled liquid radiation curable resin compositions for additive fabrication

Non-Patent Citations (1)

* Cited by examiner, ā€  Cited by third party
Title
None *

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